CN102079381A - End-to-end double-aircraft carrier battle group - Google Patents
End-to-end double-aircraft carrier battle group Download PDFInfo
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- CN102079381A CN102079381A CN2010102994545A CN201010299454A CN102079381A CN 102079381 A CN102079381 A CN 102079381A CN 2010102994545 A CN2010102994545 A CN 2010102994545A CN 201010299454 A CN201010299454 A CN 201010299454A CN 102079381 A CN102079381 A CN 102079381A
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Abstract
The invention provides an end-to-end double-aircraft carrier battle group which comprises a main aircraft carrier and an auxiliary aircraft carrier, wherein one to two penetrating type takeoff and landing runways running from an aircraft carrier tail to an aircraft carrier head are arranged between the main aircraft carrier and the auxiliary aircraft carrier; two sides of the penetrating type takeoff and landing runway are respectively provided with an inclined takeoff runway; both ends of the penetrating type takeoff and landing runway are hinged with a hydraulic lengthened takeoff and landing runway by a hinge; the piston end of a hydraulic cylinder is connected to the bottom of the hydraulic lengthening takeoff and landing runway; the hydraulic cylinder is connected with hulls of the main aircraft carrier and the auxiliary aircraft carrier; the tail of the main aircraft carrier and the head of the auxiliary aircraft carrier are connected together by the hydraulic lengthening takeoff and landing runway; the tail of the main aircraft carrier and the head of the auxiliary aircraft carrier are connected by a tensioning steel cable; and aircraft carrier islands of the main aircraft carrier and the auxiliary aircraft carrier are arranged between the two penetrating type takeoff and landing runways.
Description
Technical field
The present invention relates to a kind of large-scale marine military equipment, the two aircraft-carrier battle groups of specifically a kind of head and the tail bonded assembly.
Background technology
As everyone knows, aircraft carrier is marine airport of moving, and is the open-ocean operations platform, 332.9 meters of the maximum Nimitz level aircraft carrier captains of the known U.S., and warship is wide 40.8 meters, absorb water 11.3 meters, and what long 100-130 rice landing was gone in catapult-assisted take-off goes to 120-150 rice.General fixed wing aircraft takeoff runway is 200m-800m.F-15 is 275m, if be with three additional fuel tanks with regard to long near 300m, the J10 of China, with F-15 be a type, single-shot weighs 22 tons, Su-27, full oil will run 670m.About the about 250m of F-22, Su-33 takes off on the sliding formula runway that jumps, and the long 90-100 rice of runway is if the plane runway approximately is a 150-200 rice without ejector.China is the territory defender strategy, and China does not have aircraft carrier at present, also is that the South Sea or the East Sea type of being on the defensive in China cruises even have in for a long time; the above-mentioned aircraft carrier of prior art; ubiquitous deficiency is, can only use carrier-borne aircraft, and other fixed wing aircrafts can not landing on aircraft carrier.And carrier-borne aircraft can only could implemented landing when aircraft carrier navigates by water at a high speed.
Summary of the invention
The purpose of this invention is to provide the two aircraft-carrier battle groups of a kind of land airplane and aircraft carrier general-duty head and the tail bonded assembly; the fixed wing aircraft that is the continental rise airport also can landing on the sea base aircraft carrier, during the aircraft carrier night sky on the continental rise airport combined operation system of landing.
The objective of the invention is to realize in the following manner, comprise main aircraft carrier and auxiliary aircraft carrier, the centre of main aircraft carrier and auxiliary aircraft carrier is provided with the through landing runway of 1-2 bar from the stern to the bow, the both sides of through landing runway are provided with an oblique takeoff runway, there is hydraulic pressure lengthening landing runway at the two ends of through landing runway by hinge links, the piston end of hydraulic actuating cylinder is connected the bottom of hydraulic pressure lengthening landing runway, hydraulic actuating cylinder is connected with the hull of main aircraft carrier and auxiliary aircraft carrier, the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier link together by hydraulic pressure lengthening landing runway, also be provided with the tension cable wire between the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier, the warship island of main aircraft carrier and auxiliary aircraft carrier be arranged on two through landing runways the centre.Connecting the afterbody of main aircraft carrier and the hydraulic pressure lengthening landing runway end of auxiliary aircraft carrier is plugged on together by Connector Clip.
Excellent effect of the present invention is, the method of hydraulic pressure lengthening landing runway is set by two warship series connection and employing head and the tail, effectively improved the length of aircraft carrier, can be static provide marine landing for various opportunities of combat at sea, form the marine associating air battle in land system fast, the territorial sky, territorial waters that constantly effectively safeguards one's country is inviolable.
Description of drawings
Accompanying drawing 1 is the structural representation of the two aircraft-carrier battle groups of a kind of head and the tail bonded assembly;
Accompanying drawing 2 is the structural representation of the two aircraft-carrier battle groups of a kind of head and the tail bonded assembly;
Description of drawings: main aircraft carrier and auxiliary aircraft carrier 1, hydraulic actuating cylinder 2, hydraulic pressure lengthening landing runway 3, tension cable wire 4, oblique takeoff runway 5, through landing runway 6, warship island 7.
The specific embodiment
With reference to Figure of description to explaining below the work of the present invention.
The two aircraft-carrier battle groups of a kind of head and the tail bonded assembly of the present invention, its structure is that main aircraft carrier and auxiliary aircraft carrier 1 are formed, the centre of main aircraft carrier and auxiliary aircraft carrier 1 is provided with the through landing runway 6 of 1-2 bar from the stern to the bow, the both sides of through landing runway 6 are provided with an oblique takeoff runway 5, there is hydraulic pressure lengthening landing runway 3 at the two ends of through landing runway 6 by hinge links, the piston end of hydraulic actuating cylinder 2 is connected the bottom of hydraulic pressure lengthening landing runway 3, hydraulic actuating cylinder 2 is connected with the hull of main aircraft carrier with auxiliary aircraft carrier 1, the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier link together by hydraulic pressure lengthening landing runway 3, also be provided with tension cable wire 4 between the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier, the warship island 7 of main aircraft carrier and auxiliary aircraft carrier 1 is arranged on the centre of two through landing runways 6.
Connecting the afterbody of main aircraft carrier and hydraulic pressure lengthening landing runway 3 ends of auxiliary aircraft carrier is plugged on together by Connector Clip.Tiltedly be provided with ejector and landing retarder on takeoff runway 5 and the through landing runway 6.
Embodiment 1: the two aircraft-carrier battle groups of head and the tail bonded assembly of the present invention, the aircraft carrier main body is by 350 meters designs, each presses 30 meters designs hydraulic pressure lengthening landing runway, during length overall 410 meters, when South China Sea list ship cruises, through landing runway can provide landing at 350 meters with interior aircraft for take off distance, the roadbed aircraft can take off from airfield and cruise, postcombustion lands on the aircraft carrier, return airfield after finishing the work, this kind mode can be replenished the war note and provide air battle to support for aircraft carrier in wartime by airfield.At present, owing to do not have aircraft carrier and a staging post, the aircraft of China takes off from the continent, must hasten to make a return voyage in the Nansha of cruising, and does not have enough fuel to cruise at all or participates in air battle.Even use air refuelling, tanker aircraft are easy to be subjected to the attack of surface-to-air ballistic missile or air-to-air missile, aircraft carrier is just different, because aircraft carrier has complete prevention and control system and operation system.
Embodiment 2: when the two aircraft-carrier battle groups of head and the tail bonded assembly of the present invention cruised at the two ships of South China Sea, two aircraft carriers connected from beginning to end, form a marine floating aerodrome, and total length can reach 820 meters, can provide the landing operation for the fighter plane of all models number.If the displacement of every aircraft carrier is more than 100,000 tons, the warship body is subjected to the influence of wave very little, and two bow tail washings press the fluctuating of lengthening landing runway point of connection to ignore, and slightly diff-H can solve by the hydraulic stem adjustment.
Embodiment 3: during use, the hydraulic pressure of bow lengthening landing runway can suitably be steeved, for aircraft provides the suitable elevation angle; The hydraulic pressure of stern lengthening landing runway can suitably following hectare, for aircraft landing provides protection.
Except that the described technical characterictic of specification sheets, be the known technology of those skilled in the art.
Claims (2)
1. two aircraft-carrier battle groups of head and the tail bonded assembly, it is characterized in that, comprise main aircraft carrier and auxiliary aircraft carrier, the centre of main aircraft carrier and auxiliary aircraft carrier is provided with the through landing runway of 1-2 bar from the stern to the bow, the both sides of through landing runway are provided with an oblique takeoff runway, there is hydraulic pressure lengthening landing runway at the two ends of through landing runway by hinge links, the piston end of hydraulic actuating cylinder is connected the bottom of hydraulic pressure lengthening landing runway, hydraulic actuating cylinder is connected with the hull of main aircraft carrier and auxiliary aircraft carrier, the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier link together by hydraulic pressure lengthening landing runway, be connected by the tension cable wire between the afterbody of main aircraft carrier and the stem of auxiliary aircraft carrier, the warship island of main aircraft carrier and auxiliary aircraft carrier be arranged on two through landing runways the centre.
2. method according to claim 1 is characterized in that, connects the afterbody of main aircraft carrier and the hydraulic pressure lengthening landing runway end of auxiliary aircraft carrier and is plugged on together by Connector Clip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102994545A CN102079381A (en) | 2010-10-08 | 2010-10-08 | End-to-end double-aircraft carrier battle group |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102994545A CN102079381A (en) | 2010-10-08 | 2010-10-08 | End-to-end double-aircraft carrier battle group |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102079381A true CN102079381A (en) | 2011-06-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102994545A Pending CN102079381A (en) | 2010-10-08 | 2010-10-08 | End-to-end double-aircraft carrier battle group |
Country Status (1)
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114787A (en) * | 2014-04-30 | 2016-11-16 | 王海龙 | Combination type aircraft carrier |
| CN110588930A (en) * | 2019-09-16 | 2019-12-20 | 青岛度丘新能源技术有限公司 | Aircraft take-off and landing platform of aircraft carrier or large ship |
| CN111572740A (en) * | 2020-05-25 | 2020-08-25 | 卿先觉 | Aircraft carrier |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03112494U (en) * | 1990-03-06 | 1991-11-18 | ||
| CN1291572A (en) * | 1999-10-12 | 2001-04-18 | 张承普 | Combined aircraft carrier |
| CN101259876A (en) * | 2007-03-07 | 2008-09-10 | 左学禹 | Building block type aircraft carrier |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
-
2010
- 2010-10-08 CN CN2010102994545A patent/CN102079381A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03112494U (en) * | 1990-03-06 | 1991-11-18 | ||
| CN1291572A (en) * | 1999-10-12 | 2001-04-18 | 张承普 | Combined aircraft carrier |
| CN101259876A (en) * | 2007-03-07 | 2008-09-10 | 左学禹 | Building block type aircraft carrier |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
Non-Patent Citations (2)
| Title |
|---|
| 《国际展望》 20001130 张岳 "组合式航母"可以成为中国的"国情航母" 52-53 1-2 , 第407期 * |
| 张岳: ""组合式航母"可以成为中国的"国情航母"", 《国际展望》 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114787A (en) * | 2014-04-30 | 2016-11-16 | 王海龙 | Combination type aircraft carrier |
| CN106114786A (en) * | 2014-04-30 | 2016-11-16 | 王海龙 | Combination type aircraft carrier |
| CN106114786B (en) * | 2014-04-30 | 2017-11-07 | 王海龙 | Combined type aircraft carrier |
| CN106114787B (en) * | 2014-04-30 | 2017-12-05 | 王海龙 | Combined type aircraft carrier |
| CN110588930A (en) * | 2019-09-16 | 2019-12-20 | 青岛度丘新能源技术有限公司 | Aircraft take-off and landing platform of aircraft carrier or large ship |
| CN111572740A (en) * | 2020-05-25 | 2020-08-25 | 卿先觉 | Aircraft carrier |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20110601 |
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| RJ01 | Rejection of invention patent application after publication |